Stabilized celestial navigation instrument



June 24, 1953 F. H. HAGNER 2,339,333

STABILIZED CELESTIAL NAVIGATION INSTRUMENT Filed March 26, 1952 I 5 Sheets-Sheet 1 INVENTOR Ewan/m A. Aha/via #15 ATTORNEY June 24, 1958 F. H. HAGNER STABILIZED CELESTIAL NAVIGATION INSTRUMEN Filed March 26, 1952 5 Sheets-Sheet 2 ///5- ATTORNEY June 1958 F. H. HAGNER 2,839,833

STABILIZED CELESTIAL NAVIGATION INSTRUMENT Filed March 26, 1952 3 Sheets-Sheet 3 0/8 ATTORNEY l [STABILIZED 2 ,s39,s33'- CELESTIA-LNAVIGATION" V INSTRUMENT Frederick Hag'ner, San Antonio, Tex.

Application March 26,1952, Serial No, 278,598 I 1 The object of this invention is to produce ast'ahilized means upon Which-an observing instrument or an aerial camera may be mounted so' as tobe free from vibration. Another'object of this' invention is to provide a means to-facilitate the moving of an instrument or aerial camera in azimuth (horizontal plane) without touching the stabilizer' ortlre device it: supports. Another-object of this invention is 'to reproduce the necessary'arc's of the-celestial sphere upon which arcs telesco'pes=br"sighting devices are mounted and set on scales to represent the relationship of two or more celes-- tia'l bodies-as these "bodies will appear on the celestial spherefor agiven date and time.

Another object of this'nvention is to provide a simple means to facilitate slow movement of the sighting devices while training thenr in' simultaneous "alignment with celestial bodies 'in'the' sky. v Another'objectof this invention ris no record the movement of theinstrument in azimuth (horizontalplane) and around a zenith pointinthe sky: (ima'ginary),' dur- ,iingthe time of observation :by the operator.

-. 1 Another :objectofithis.'nvention is-to attach the entire unit to the aircraft or ship-so as toghave a reference of :the

heading o'fEthet -craft. j 1 A1l0th6fobject-of this invention is ;-to provide an optical arrangement whereby the observer may sight two a celestial bodies-or objects at wide angles from each other atthe same time;

Unite SW68 Pa 1 "i e Another object of this invention is to provide-references in the-;-sigh ting-un its of the instrument which enable the floperator to z-lgnow which are has been moved.

- A furthers-object of the invention, is the provision ofv a celestial observation instrument having vscales and sighting units-wherein thesightirig unitsmaybepre-set onthe scalesforz a definite location on a-scourse being arthfs surface to enable anobserver to wihe raters ment llif 'the image or the celestial body ob- Another object of'thi's invention is to prov'i'de antn'str ur'ne rit-suitab le for observation 'ofe-hig'h'altitude-stars and planets duringday time,"the' instrumeht' being constructedsthattwo stars will be within the new of the telescopeswhe'n t-he telescopes are';proper1y:set 1 Another ;object; {of thiswinventlon {is to provide can instrument to determine theorientationofithe -celestial sphere,tron pole tqpole, and to define thi orientation in .terms which' will correspond ;to latitude .andslongitude, f

I ention is t he prodiiction o'f'a 'celes'tial'obs'er'vation' instrument having arcs Al s'tilljfiur'ther'object of the present,

in Figure ,10;

1 of the Polaris telescope; telescope showing'the index and scale therefor; 0

cam of the Polaristelfescope;

2,839,833 Patented June 24, 19 58 provided with scales upon which information obtained from the nautical or air almanacs is carried and wherein.

the sighting units are selectively and properly set after the instrument .is properly mounted in an aircraft 'or ships charthouse with reference to the planes' 'or ships heading reference, to" give .to an observer, the relationship as'to distance between' 'two observed bodiesas represented by the respective positions of the sighting units Another object of "this invention is to produce 'an instrument having a j gravity controlled leveling reference with scalesin minutesof arc, the scales being ada to be moved from the center '(representing'zenith) toa os ition obtained mm the Coriolis Ac'celerationco'rr tion tables in the AirAlman'ac published by the Us. aval Observatory, to automaticallycornpensate fo'r jthe error 'at the latitude where" the plane is in flight and fthe speed and direction it is traveling over the earths surface. Another object of this invention is the production of a simple and eflicient "r'neansfo'r simultaneously me sining the angles of the'rays of light from two celestial bodies-or objects with respect'to the position of an observer and simultaneously recbrdingthe' motion between the instrument and the-aircraft or ship upon which the instrument is, mounted.

"other objects and "advantages "of the present invention will appear throughout the following specification and claims. 1 I

This application is a continuation in part of my'application relating to a Celestial Observation Instrument, Serial Number 617,636, filed September 20, 1945', and now abandoned. J 1 F g In thedrawings.: v t Figure 1 is a side elevational view of the instrument Witlithe telescope supporting 'arcs in a substantially vertical position; a .s v, 4 Figure 2 isa top plan view of the instrument with-the .telescope'supporting arcs atdiverging angles;

t Figure 3 is a central: vertical sectional view taken-lat right-angles to Figure 1;

Figure 4 is an irregular'ho'rizontal sectional view taken Figure 5 is a side elevational-view,= partly in section of one type of telescope or sighting unit;

- Figure 5 is a sectional ;view of a modified form-of t-he viewing mirrortwhich may replace the :mirror s'hownin Figure 5;

Figure 6 is anend view of one of the telescopes or .sightingunits such'as is shown in Figure 5;

Figure 7 is a'fragmentary'sectional view of the float; Figure 8 is-a vertical sectionalvview of amodified form V of one of theslides which supports one ofthetelescopes,

certain'partsbeing shown in elevation; a 1

Figure 9 is a fragmentary top plan view of the structure shown in Figurex8, certain parts-beingeshowntin section; a Y Y Figure IO-is a ve rtical sectionallview partly in section o tmQ ifi df m-Q ing-u t;

g Figure 1 1 is a top plan view of the. sighting unitshown FigureQIlZ is a horizontal sectional view taken on line 12.-- 12 of Figure. 10; 1

Figure l3is a side elevat-ional view, partly in section,

Figure 14 is .a side elevational view of the Polaris vFigure 15 is a front vi w of the primary SeGtlOlip kite ' Figure 116 is In ,endtpelevatil nal view of Polaris telescope in one position the eye-piece being broken away; v a; v Figure l7 is 'anend elevational view of the Polaris ships heading, and to determine the true north to the ships heading.

, The float 23 carries a plurality of upwardly extending "ieis cope in an adjusted position, the eye-piece being broken away; I

Figure 18 is a fragmentary bottom plan view of the Polaris telescope showing the sections of the cam separated;

Figure 19 is a fragmentary top plan view of the Polaris telescope showing the sections of the cam separated.-

By'referring to the. drawings in detail, itwill be seen that 15 designates the base which is fixed to a suitable support such as'a ship, aircraft, and the like, or the base 15may. be mounted upon a conventional support which is adjustable as to tilt, if desired. The base 15 .supports a shallow bowl-like body 16.having a concavolconvex outer wall 17 and a similar inner or inwardly spac edwall 18 defining an outer liquid containing com- ...partrnent 19 and an inner balancing and recording com- ,rpartment 20. The body and base preferably are moulded of- Jone-piece transparent plastic material. 7

I A band 21 is fitted around the outer wall 17 of the body 16,;and is movable in azimuth around the body 16. This band 21 carries diametrically spacedvertically extending-plates 21% having maximum magnetic attracting characteristics, such as softiron, or the like.

The compartment 19 contains a suitable quantity of .mercury 19 orother vibration dampening material, such asoil-or the like. Thebody' 16, when not in use, may

be covered at its open upperend by a suitable removable cap or cover 22, a part of ,which isshown in Fig-, sure 1, to prevent the mercury or, other liquid from spilling out of the compartment 19 when the superstructure is removed and the instrument is not in use. The cover -or cap 22 is adapted to completely cover the body 16. .-The base may bemounted upon, conventional gimbals 114, as is shownin Figure 1. Y

type float 23 is placed When in use, a circular or other within the compartment 19 to rest upon the liquid or .mercury 19, as shownin Figure 3, to support the float $23; The float carries a plurality of bearings 24 suitably located to contact the inner face of the wall 17 to eliminatetfriction. The float .23 is hollow and preferably contains a colored liquid 25,.light asto weight. A dia- The the liquid within the tube or tubes 26*. The float'23 is spacedfromthe wall 18 as well as'from the wall 17.

The float 23 is graduated 360 near-"its periph ryyat "23 andcarries' a suitable permanentmagnct or preferably a plurality of 'magnets such as the two magnets 28,, to match the numbera of plates 21 which are carried by the band 2 l. The magnets 28-in conjunction with the plates 21 permit the rotation of the float 23- asthe band 21 is' rotated by the observer, buttend to retain the float in'its normal position. Themagnetic =fiux between the plates- 21 and the magnets 28 constitutes an invisible connection between the float 23 and the band 21, and causesthe float 23'to rotate inunison The band 21 is transparent and an i index arrow 29'isicar'ried by the outerface of the wall with the band 21.

17 near its upper edge, so thatthe position of the ,scale 23 of thefloat 23in azimuth may be read with respect to this index 29, which index 29 designates the Ships --Heading. Since'the" wa1i11, is transparent, the'degre'es on the 1 float 23 maybe easily read by the; observer -'-throu gh"the wall 17 to 'determinethe position of the float in degrees in azimuth relativetd the .index"29,the e relative bearing of arms 30 which support gimbal rings 31 of the conventional 'type which are commonly used to obtain a universal movement.

A carriage cradle 32 is suspended from the inner ring of the gimbal rings 31 by means of arms 32. A pendulum or weight 33 is suspended from the cradle 32, and carries a pivoted stylus 34 at its lower end which may be swung into and out of an operative position to mark or record the position of the pendulum 33 upon the zenith recording chart35, carried within the compartment 20 belowthe pendulum 33. An azimuth indicating arm 36 is carried by the pendulum 33 intermediate its ends and extends at right-angles to the pendulum 33. The arm 36 carries a pivoted stylus 37 of suitable marking material, and which may be swung into and out of an operative position, for marking on the inner face of the wall 18 to indicate the amount of motion of the instrument during the time of observation. A suitable counter balance weight 38 iswcarried by the pendulum 33. A graduated arm39 extends. at rightangles to the pendulum 33 .and an adjustable weight 40 is slidable'upon the arm 39 to counteract the effect of Coriolis, Coriolis is defined as the acceleration, due to the rate of change in the straight line and due to the curvature of the earth in rotation under (for. example) the moving ship. This acceleration is a function of the latitude in which the ship is located and:the speed at which the ship is moving. The effect .ofgCoriolis is to tilt the level or mercury by a definite: amount normal to the ships heading, Thisflamountcan be found and tabulatedin a table found in tthe .AirgAlmanac published by-the Naval Observatory, and: having .as' arguments, the latitude, and the speed-ofthe ship.

Suitable level references 41 and 42;. ofatype as disclosed in my Patent No.: 2,557,654, issued June 19,1951, relating to a Direction Inclination. Indicatorgare preferably carried by'thegimbalrings31'. 3 A latitude are. 43 graduated-90 north and 90 south latitude is slidably mounted within the-cradle 32. At the zeropoint at opposite endsof- -the" are-43 are fixed inwardly extending bearing shafts 44 and 45. -The are 43, during observation, normally extends due north and south and the shafts 44 and 45 represent the axes of the *earth. The cradle 32is provided with' -index"lines 46 and 47, 180 apart, extending in line center of the-instrument. I

At the point'on the latitude arc-43' and extending at right-angles-thereto, a second cradle*48"is mounted and secured to the latitude arc 43 by means'of a stud 50. A local hour angle are 49, graduated from zero-at its center to 90 toward either end, is slidably mounted with thegeometric i in the cradle48. A declination a'rc 51ispiv'oted at the tit) poles on'shafts 44 and 45 which' extend airtight-angles to the latitude are 43. This are 51 is graduated starting at. zero in the .center, the celestial equator,'to 90 toward eachpole orthe shafts 44 and 45; The declination are 51 is connected to-one end of the hour angle arc 49a! its zero point intermediate the ends of'the are 51. A.

movable slide 52 carrying a suitable sighting device 53, telescope, etc., is slidably mounted in any desired manner upon'the declination are 51, to be moved and set in a selected position within the radius of the are 51, to represent the declination of a selected celestial body; as listed in the Nautical Almanac fora given date and time.

Asidereal hour angle difference are 54 is slidably mounted within the. local hour angle arc.49, which ,is

7 carried by the cradle .48 and is adjustable circumferentially around the axes of the shafts 44 and 45, as will be obvious by considering Figure 3. This are 54is graduated' from zero to about more or less, toward each end-for measuring 'the-sidereal hour'ang'le'diffe'rence Almanac, relating to the'selectedacelestial bOdiCS'itO be observed. I

A second declination are 55 similar to "the are '51., also is pivoted on the shafts or .poles '44 and 45, as shown in Figure 1. This are 55:is graduated from zero at its center, the celestial equator, to 90 toward each end or pole. A movable slide 56 carrying a suitable sighting device 57, telescope, etc., is .slidably timounted in any desired manner uponthe second declination are 55. This slide maybe moved and set in a selected position within the radius of the arc55, to indicate the declination of the celestial body which'is obtained from the Nautical Almanac. e

As shown in Figures 5 and 6 the sighting device 53 is adjustable in the conventional manner, and is mounted so that its longitudinal axis radiates from the central axis of the instrument. An arm 58 is adjustable longitudinally of the telescope '53 and carries at one end thereof a universally mounted mirror 59 to reflect an image of a celestial body, the rays of light from which pass throughthe-te'lescope 53. The telescope 57 is similar to the telescope 5 3, and carries a universally mounted mirror 60 similar to the mirror 59. The telescope 57 is mounted upon the are 55 so that the longitudinal axis of the :arc radiates from the central axis of the instrument in a similar manner to that described with respect to the telescope 53. If desired, the mirror may be convex in cross-section as shown at 59 to increase the viewing angle thereof and permit images from both sighting devices 53 and"57 to be reflected from one mirror, if desired. i a

The mounting of the telescopes '53 and 57, asshown, permits an observer to bring'the images of two celestial bodies within the limited range of vision of an observer so that the images may be simultaneously and conveniently viewed although the actual celestial bodies are at a great angular distance from each other. 'When two selected celestial bodies are in columnation with respective telescopes, and the instrument is .in a mean level'position, the reading on the scales are as follows-:'

(l) Latitude scale 43 will give the observers latitude, for instance, latitude 40 north; 1

(2) The azimuth scale 23 on the float-opposite the ships heading reference 29 indicates 'the ships heading at the time of observation, e. g., 90;

(3) The local hour angle'onlocal angle arc 49 indicates the local hour angle measurement of the-slide "51 and the telescope 53, to give the local'hour angle east or west of the observers meridian, of the observed body. Should the observed body be east of the observersmeridian,the reading on the scale is added to the Greenwich hour angle of the celestial body given in the Nautical Almanac for the date :and time of observation. The'answ'er is the observers longitude. If the observed body is west 'of'the observers meridian the reading on the local hour'ang'le scale 49 is subtracted from the Almanac date for the time and date of observation to give the observers longitude.

For instance, when the reading 45 E. on the scale and the Almanac date shows the Greenwich hour angle as 30 for time of observation the longitude would be 75.

The one measurement of the local hour angle is allthat is necessary to obtain the longitude of; the observer.

It should be noted that when making the observation the relative angles of the declination arcs are fixed by means of the set screw 61 to lock these arcs togethenf" 'I=o align the celestial bodies, the observe 'r 'slides the latitude arc 43 in the cradle 32, which is always a north and south motion, to bring both bodies within the range of the respective telescopes. The movement of the local hour angle 49, which is an east and west.movement, in conjunction with the rotatable. movement of the band 16 in a substantially horizontal .plane resultingin the rotation of the float 23 will'bring the telescopes 53 and 57 into columnation with the selected bodies.. The images of these bodies will be reflected on the mirrors 45 and 60. Before making observation, the instrument is balanced in a level position. In'order to obtain a record "of the motions taking place during the period of observation, the observer moves thetwo styluses'34 and 37 to an operative'positiomwhich styluses'may be swung into and out of an operative position because of their pivotal mounting as shown. The movement in azimuth is recorded on the inner face of the. wall 18, to indicate the relative movement between the heading of the airplane or ship and the north point-on the instrument. The angular movement with reference to zenith is recorded by the stylus 34 on the chart 35.

The mercury 19 supports the measuring elements of the instrument in floating relation with respect to the body 16, and the mercury dampens vibration caused by the ship or plane upon which the instrument is mounted.

It is a known fact that stars are visible by use of a high- I powered telescope, such as is used in the present instance,

mercury supported float and associated mechanism.

In Figures 10 to 12, there is shown a modified form of sighting device which comprises a pair of aligned reticles '65 and 66 having sight registering cross wires 67 and 68 of the conventional type. These reticles are mounted in a housing 69, which housing fits through the slotted supporting arc, such as the declination arcs 51 and 55. The

housing 69 carries a depending arm 70 having an adjustable end extension 71. A mirror 72 is carried by the lower end of the extension 71 and ispivotally mounted so asto. swing in two-right-angular directions. The mirror comprises an outer band pivoted, as at 73, to the extension 71, and aninner band-carrying the reflected surface pivoted within the outer band at right-angles to the pivot As shown in Figures 8 and 9, the sighting device 74, similar to the sighting device 56, is slidably mounted upon the declination are 75 by means of a housing 76.- A vernier 77 is carried by the housing 76 for meshing engagement with suitable teeth 75 carried by the are 75. It should be understood that a vernier may be used foradjustment of any of the arcs of the instrument within the spirit of the invention, and since verniers are commonly used for such adjustments, it is thought unnecessary to illustrate and describe in detail such vernier connections.

The mounting of a vernier to provide adjustment is well.

- 78 is supported. by a suitable bracket 79, which is detachably secured to the latitude are 43 as above described. The telescope 78 rotates on anaxis in line with the polar axis of the instrument, that is, the axis of the shaft 45.

As is shown in Figures 13, 14 and 15, the'bracket 79 carries a journal bolt 80 which constitutes the axis of the shaft 45, upon which is rotatablyrnounted theprimary section 81 of an adjustment cam 82. An auxiliary section 83 ofthe adjustment cam 82 is also rotatably mounted upon the journal bolt 80. The section 81 is provided with a plurality'of sockets 84 arranged in an encircling path aroundthe bolt 80. A spring-pressed ball 85 is carried by the auxiliary s'ection83 and normally engages one selected socket 84in the primary section 81. This spring-pressed balland the sockets provide a releasable latching means upon the meeting faces of the cams to detachably hold J the auxiliary section 83 in a selected rotated position with respect to the cam section 81. An index'85 is carried by one. section of the cam for registration with the rotation,' manual' orotherwise.

made, to thereby measure an observers latitude, the rela- 5 scale 86 which is carried by the companionsectionof the cam to indicate the position of Polaris in its changing of arc variation necessary to correct the daily change of position of Polaris around the true celestial pole. For

correcting an observation of the star Polaris to determine theiobservers latitude on the earth and the true celestial north point, the section 83 is rotated to the proper position upon the section 81 to change the angular position of the a telescope 87 and to make the necessary correction as provided in the table found in the Nautical Almanac. This celestial north point is absolutely necessary for correcting compasses and establishing geographic surveys on the earths surface. A right-angular telescopic element 87 of a conventional type is fixed to the cam section 83 and is rotatable with the cam section 83 after being corrected mechanically to take care of the variance in minutes of are relative to Polaris and the true celestial pole. The

' telescopic element 87 is provided with a reticle 88 and the telescopic element 87 may be rotated with both cam sections360 around the line of sight.

The use of thePolaris telescope:

ExampIe.Polaris appears from observer to rotate 1 ofi center from the true celestial pole. The correction for this rotating motion is listed in Nautical Almanac issued by the'Naval Observatory. By rotating the cam section 83 to bring the index Polaris intoregistration' with point 9 P. M.

" on the scale'see Figure l8"located on cam section 82 which is the position of Polaris at the time of sight, in referenceto the true celestial pole, the'angle of tilt of the telescope 87 with this setting automatically gives the true latitude and true north point on the latitude arc 43 and the azimuth scale 23: with reference to the ships or planes heading 29 when the instrument is level and the reticle of the telescope 87 is in registration with Polaris.

The operation of this device eliminates calculations to determine the observer's latitude and the true heading of the ship or plane as is now necessary with instruments now in use. Up tolthis time mathematical calculation, using 'information'obtained from the Nautical Almanac published by the Naval Observatory, has been necessary to make these corrections. By means of the present device, the corrections are made mechanically bychanging the incline of the telescope 87 to match the 1 otf center position of, Polaris relative to the true celestial north and the obs'ervers latitude -with respect to the earth. The cam section 83 may be rotatcdrrelative to the cam section 82 to periodically change the angular tilt of the telescope '87 with reference to the'continuous change in geographic position of the instrument upon which the Polaris telescope is carried. Any. means maybe provided for this Through the' mediurn of the arcs 51 and 55, and the sighting devices 53 and 57, a means is provided for setting two sighting devices on .arcs representing the celestial "sphere and matching the" rays of light from 'two stars,

through the sighting devices after the settings have been tive bearing of'the ships heading to. true north, and the local hour angle of one of the stars which is matched.

Having described the invention, what I claim as new is: '1. An instrument of the class described comprising a base, a pair of sighting devices, measuring means for measuring the angular positions" of said sighting Ydevices relative to said base and relative to each other, and said sighting devices being adjustably mounted relative to said base and to each other to bring the images of two, celestial bodies simultaneously within the range of vision measuring means having a polar axis, and a Polaris telefrom said instrument to determine it adjusting meanscarried by the body and rotatable about :the central'axis of .the body, co-acting magnetic means carried .by said float and said float-adjusting means and providing an invisible connection therebetween to facilitate the rotative adjustment of the float as the floatatijusting m'eans'is moved circumferentially of the "body,

means carried ,by the gimbal rings for measuring the angle of the ray of light from a celestial body with respect to saidinstrument, said body having a recording compartmentinwardlyof the liquid'containing compartment, a pendulum hung, from said gimbalrings, and recording means carried by said recording compartment :andpendulum for recording the position of the means for measuring, the angle of a ray of light with respect to zenith at the time of observation.

3. An instrument of the class described comprising a base,.a bowl-like body carried by the base, said body having a liquid-containing compartment, a float in said compartment, gimbal rings mounted upon said float, a float adjusting means carried by the body and rotatable about -the central axis of thebody, co-acting magnetic means carried by said float and said float-adjusting means and providing an invisible connection therebetween to facilitate the rotative adjustment of the float as the float-adjusting means is moved circumferentially ofthe body,

ment, a pendulum hung from said gimba'l rings, recording means carried by said recording compartment and pendulum for recording the position of the means for measuring the angle of a ray of light with respect. to Zenith .at the time of observation, said recording means comprising a chart carried by the recording compartment,

and a stylus carried by the pendulum. ,7

4. An instrument of the class described comprising a base, a bowl-like body carried by the base, said body having a liquid-containing compartment, a float in said compartment, gimbal rings mounted upon said float, a float adjusting means carried by the body and rotatable about the central axis of the body, co-acting magnetic means carried by said float and said float-adjusting means and providing an invisible connection therebetween to facilitate the. rotative adjustment of the float as the floatadjusting means is moved circumferentially of the body, means carried by the gimbal rings for measuringvthe angle of the ray of light from a celestial body with respect to said instrument, said body having a recording compartment inwardly of the liquid-containing,compartment, a pendulum hung from said gimbal rings, recording means carried by said recordingcompartment and pendulum for recording the position of the means for measuring the, angle of .a ray of light with respect to zenith'at the time of observation, and an azimuth ing means carried by said pendulum. ,7

5. An instrument of the class described comprising a base, a bowl-like body carried by the base, said body having a liquid-containing compartment, a float in said compartment, gimbal rings mounted upon said float, a float position record- -adjusting means carried by the body and rotatable about the. central axis of the body, co-acting magnetic means -carried by said float and'said float-adjusting means and providing an invisible connection therebet'ween ,to facili- T'tate the rotative adjustmentof the float as the float-adjust ing means is moved-circumferentially ofthe body,

means carried by the gimbal rings for measuring the angle of the ray of light from a celestial body with respect to said instrument, said body having a recording compartment inwardly of the liquid-containing compartment, a pendulum hung from said gimbal rings, recording means carried by said recording compartment and pendulum for recording the position of the means for measuring the angle of a ray of light with respect to zenith at the time of observation, an azimuth position recording means carried by said pendulum, and a weighted Coriolis correction means carried by said pendulum.

6. An instrument of the class described comprising a base, a bowl-like body carried by the base, said body having a mercury-containing compartment, mercury in said compartment, 21 float in said compartment, gimbal rings mounted upon said float, a float adjusting means carried by the body and rotatable about the central axis of the body, co-acting magnetic means carried by said float and said float-adjusting means and providing an invisible connection therebetween to facilitate the rotative adjustment of the float as the float-adjusting means is moved circumferentially of the body, means carried by the gimbal rings for measuring the angle of the ray of light from a celestial body with respect to said instrument, a diaphragm formed in the bottom of said float, a liquid in said float, and means carried by said float to register the position of said liquid in said float to indicate the angle of tilt of said float with respect to a level position.

7. In combination with an observation instrument having a latitude arc and a plurality of declination arcs journalled on the Polaris axis of said Ilatitude arc, sighting devices carried by said declination arcs for sighting celestial objects to determine the positions of said objects, and a Polaris telescope rotatably mounted upon said polar axis for observing Polaris from said instrument and determining its position with respect to an observer.

8. An instrument of the class described comprising a 7 support, a latitude are mounted upon said base and adapted to be aligned with the polar axis, a journal carried by said latitude are adapted to extend in line with the polar axis, a telescope comprising a sighting element rotatably mounted upon said journal for alignment with the polar axis, and means for changing the angular position of the sighting element relative to the polar axis to follow the daily eccentric path of Polaris around the true celestial pole. V

9. An instrument of the class described comprising a support, a latitude are mounted upon said base and adapted to be aligned with the polar axis, a journal carried by said latitude are adapted to extend in line with the polar axis, a telescope comprising a sighting element rotatably mounted upon said journal for alignment with the polar axis, means for changing the angular position of the sighting element relative to the polar axis to follow the daily eccentric path of Polaris. around the true celestial pole, said telescope comprising a pair of cam sections supporting the telescope, and means for locking the cam sections in relative adjusted relation.

10. An instrument of the class described comprising a support, a latitude are mounted upon said base and adapted to be aligned with the polar axis, a journal carried by said latitude are adapted toextend in line with the polar axis, a telescope comprising a sighting element rotatably mounted upon said journal for alignment with the polar axis, means for changing the angular position of the sighting element relative to the polar axis to follow the daily eccentric path of Polaris around the true celestial pole, said telescope comprising a pair of cam sections supporting the telescope, means for locking the cam sections in relative adjusted relation, and indicating means on the cam sections to indicate the adjusted position of the sections and the telescope carried thereby.

11. An instrument of the class described comprising a hollow base having a float receiving chamber, a compartment on said base within said chamber, a fluent material between the walls of said chamber and said compartment, a float supported by said material, means supported upon said float for measuring the position of celestial objects relative to an observer, and means suspended below said first mentioned means and positioned within said compartment for compensating for the force of Coriolis.

12. An instrument of the class described comprising a hollow base having a float receiving chamber, a compartment on said base within said chamber, a fluent material between the walls of said chamber and said compartment, a float supported by said material, means supported upon said float for measuring the position of celestial objects relative to an observer, and means suspended below said first mentioned means and positioned within said compartment for counterbalancing the entire instrument. 7

13. An instrument of the class described comprising a hollow base having a float receiving chamber, a compartment on said base within said chamber, a fluent material between the walls of said chamberand said compartment, a float supported by said material, means supported upon said float for measuring the position of celestial objects relative to an observer, and means suspended below said first mentioned means and positioned within said compartment for recording an azimuth reading.

14. An instrument of the class described comprising a hollow base having a float receiving chamber, a compartment on said base within said chamber, a fluent material between the walls of said chamber and said compartment, a float supported by said material, means supported upon said float for measuring the position of celestial objects relative to an observer, and means suspended below said first mentioned means and positioned within said compartment for recording an azimuth reference.

15. An instrument of the class described comprising a base having an outer fluid containing compartment and an inner compartment within said outer compartment, fluid contained between thewalls of said outer compartment and said inner compartmengmeasuring means supported upon said fluid in said fluid containing compartment for measuring the positions of celestial objects relative to an observer, and. a pendulum connected to and suspended below said measuring means and extending into said inner compartment of said base for free unobstructed swinging movement of said pendulum in a manner whereby said measuring means will be sensitive to.

the movement of said fluid in said outer compartment.

References Cited in the file of this patent UNITED STATES PATENTS 

